HIGH TEMPERATURE RESINS, ANALYSIS OF PROCESS PARAMETERS, AND EVALUATION PROCEDURES FOR FILAMENT WOUND COMPOSITES. PART II. ANALYSIS OF PROCESS PARAMETERS

Abstract

The principal process parameters studied were the delivery of reinforcement an resin impregnation. v ariations of the standard ECG 150 -1/0 yarn were investigated. A study of the rate of loading was conducted to determine its ef ect n laminate ultimate strength. Evaluation o the parameters was primarily accomplished by comparison of the p ysical laminate properties obtained, along with the ultimate strengths developed by biaxially loaded test specimens. The effectiveness of the application of optimun process parameters to a practical structure was investigated by the fabrication an test of everal typical rocket motor cases. In delivery, the tension magnitude an uniformity greatly in luenced both the physical and mechanical properties of the laminate. Viscosity f the resin system was the most critical parameter affecting impregnation. T e glass fiber strength o production yarn, ECG 15 -1/0, was equivalent to the same type environmentally pr tected yarn and environmentally pr tected roving. Load rate control as essential in magnitude of the failure stress and the mo e f ailure. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 01, 1962
Accession Number
AD0291897

Entities

People

  • Charles B. Kurz
  • S. Yurenka
  • Warren E. Ponemon

Tags

Communities of Interest

  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Composite Materials
  • Fabrication
  • Filaments
  • Glass Fibers
  • High Temperature
  • Impregnation
  • Laminates
  • Material Forming Processes
  • Materials Processing
  • Mechanical Properties
  • Rocket Engines
  • Test And Evaluation
  • Viscosity

Fields of Study

  • Materials science

Readers

  • Computational Modeling and Simulation
  • Reinforced Composite Materials
  • Snow Cover Descriptors for Reptiles and Their Illustrations.